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Gravity and force

Launch escape thrust of a Soyuz rocket

This is the force produced by the Soyuz rocket's launch escape system to rapidly move the crew capsule away in an emergency.

How big is it?

4 MN · force

Force · approximate
Typical recorded range: 3.8 MN to 4.2 MN.

Scale illustration of the launch escape thrust of a Soyuz rocket, showing the recorded force.
Recorded force: 4 MN.

A little perspective

Launch escape thrust of a Soyuz rocket vs Falcon 9 liftoff thrust: weight comparison

The liftoff thrust of a Falcon 9 is about 1.9 times the launch escape thrust of a Soyuz rocket.

Scale

FORCE

Launch escape thrust of a Soyuz rocket

This is the force produced by the Soyuz rocket's launch escape system to rapidly move the crew capsule away in an emergency.

4 MNForce
0
Falcon 9 liftoff thrust

Falcon 9 liftoff thrust is the total force produced by the Falcon 9 rocket's engines to lift it off the launch pad.

7.6 MNLiftoff thrust
0
Bar length measures force in newtons. Mass and local gravity determine weight.
Measurements, assumptions & sources +

Launch escape thrust of a Soyuz rocket

Force: 4 MN; approximate; range 3.8 MN–4.2 MN.

A curated launch escape thrust of a soyuz rocket comparison anchor. The representative value and any stated range preserve the backlog measurement convention; operating or experimental conditions can change real observations.

Defined examples — our methodology

The marked force is calibrated. Unmeasured illustration details are representative.

Falcon 9 liftoff thrust

Liftoff thrust: 7.6 MN; approximate; range 7.4 MN–7.8 MN.

A representative 7.6 MN sea-level liftoff-thrust anchor for a Falcon 9. Vehicle revision, engine operating point and atmospheric conditions change the actual value.

Defined examples — our methodology

The marked liftoff thrust is calibrated. Unmeasured illustration details are representative.

Use the visual comparison to explore its scale, then check the measurements and sources.

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Why this measurement?

Why we use 4 MN

We compare the launch escape thrust of a Soyuz rocket. This is an estimate; check the notes for its rounding and uncertainty. The recorded range is 3.8 MN to 4.2 MN.

A curated launch escape thrust of a soyuz rocket comparison anchor. The representative value and any stated range preserve the backlog measurement convention; operating or experimental conditions can change real observations.

The picture identifies the subject; the diagram compares the recorded values. How calibrated comparisons work →

Explore gravity and force →

Recorded properties

Dimensions and measurements

PropertySelected valueRecorded rangeBasis
4 MN3.8 MN to 4.2 MNapproximate

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Sources and method

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